Experimental Validation of a Highly Damped Deployable Solar Panel Module with a Pogo Pin-Based Burn Wire Triggering Release Mechanism

المؤلفون المشاركون

Bhattarai, Shankar
Kim, Hongrae
Oh, Hyun-Ung
Go, Ji-Seong

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2020، العدد 2020 (31 ديسمبر/كانون الأول 2020)، ص ص. 1-14، 14ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2020-12-15

دولة النشر

مصر

عدد الصفحات

14

الملخص EN

In this present work, a highly damped deployable solar panel module was developed for application in the 3 U CubeSat.

The solar panel proposed herein is effective in guaranteeing the structural safety of solar cells under a launch environment owing to the superior damping characteristics achieved using multilayered stiffeners with viscoelastic acrylic tapes.

A holding and release action of the solar panel was achieved by a new version of spring-loaded pogo pin-based burn wire triggering mechanism.

A demonstration model of high-damping solar panel assembly was fabricated and tested to validate the effectiveness of the design.

The holding and release mechanism achieved using a pogo pin was functionally tested through solar panel deployment tests under ambient room temperature and a thermal vacuum environment.

The design effectiveness and structural safety of the solar panel module were validated through qualification-level launch and in-orbit environment tests.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Bhattarai, Shankar& Go, Ji-Seong& Kim, Hongrae& Oh, Hyun-Ung. 2020. Experimental Validation of a Highly Damped Deployable Solar Panel Module with a Pogo Pin-Based Burn Wire Triggering Release Mechanism. International Journal of Aerospace Engineering،Vol. 2020, no. 2020, pp.1-14.
https://search.emarefa.net/detail/BIM-1168314

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Bhattarai, Shankar…[et al.]. Experimental Validation of a Highly Damped Deployable Solar Panel Module with a Pogo Pin-Based Burn Wire Triggering Release Mechanism. International Journal of Aerospace Engineering No. 2020 (2020), pp.1-14.
https://search.emarefa.net/detail/BIM-1168314

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Bhattarai, Shankar& Go, Ji-Seong& Kim, Hongrae& Oh, Hyun-Ung. Experimental Validation of a Highly Damped Deployable Solar Panel Module with a Pogo Pin-Based Burn Wire Triggering Release Mechanism. International Journal of Aerospace Engineering. 2020. Vol. 2020, no. 2020, pp.1-14.
https://search.emarefa.net/detail/BIM-1168314

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1168314